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 ESDU
 AERO
 W.00.03.01
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ESDU AERO W.00.03.01 53rd Edition, January 1, 1994
Critical Mach number for high speed aerofoil sections.
Includes all amendments and changes through AB, January 1, 1994

ESDU AERO W.00.03.01

53rd Edition, January 1, 1994

Complete Document
 
Critical Mach number for high speed aerofoil sections.
Includes all amendments and changes through AB, January 1, 1994
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ESDU AERO W.S.05.03.01 56th Edition, January 1, 1994
Pressure distribution on blunt noses of two-dimensional sections at zero incidence in supersonic flow.
Includes all amendments and changes through AB, January 1, 1994

ESDU AERO W.S.05.03.01

56th Edition, January 1, 1994

Complete Document
 
Pressure distribution on blunt noses of two-dimensional sections at zero incidence in supersonic flow.
Includes all amendments and changes through AB, January 1, 1994
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ESDU AERO W.S.00.03.04 54th Edition, March 1, 1995
Theoretical properties of two-dimensional supersonic aerofoils of simple section.
Includes all amendments and changes through AB, March 1, 1995

ESDU AERO W.S.00.03.04

54th Edition, March 1, 1995

Complete Document
 
Theoretical properties of two-dimensional supersonic aerofoils of simple section.
Includes all amendments and changes through AB, March 1, 1995
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ESDU AERO W.S.00.03.05 56th Edition, October 1, 1982
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO W.S.00.03.05

56th Edition, October 1, 1982

Complete Document
 
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO W.S.00.03.18 55th Edition, January 1, 1981
Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation.
Includes all amendments and changes through AB, January 1, 1981

ESDU AERO W.S.00.03.18

55th Edition, January 1, 1981

Complete Document
 
Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation.
Includes all amendments and changes through AB, January 1, 1981
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ESDU AERO W.S.00.03.03 56th Edition, October 1, 1982
Introductory Item on two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO W.S.00.03.03

56th Edition, October 1, 1982

Complete Document
 
Introductory Item on two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO 00.03.31 1965 Edition, August 1, 1965
Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum flow deflection angle.

ESDU AERO 00.03.31

1965 Edition, August 1, 1965

Complete Document
 
Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum flow deflection angle.
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ESDU AERO 00.03.28 63rd Edition, February 1, 1978
Conditions behind normal shock waves in a perfect gas for various values of gamma.
Includes all amendments and changes through AA, February 1, 1978

ESDU AERO 00.03.28

63rd Edition, February 1, 1978

Complete Document
 
Conditions behind normal shock waves in a perfect gas for various values of gamma.
Includes all amendments and changes through AA, February 1, 1978
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ESDU AERO 00.03.26 62nd Edition, April 1, 1973
Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section.
Includes all amendments and changes through AA, April 1, 1973

ESDU AERO 00.03.26

62nd Edition, April 1, 1973

Complete Document
 
Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section.
Includes all amendments and changes through AA, April 1, 1973
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ESDU AERO 00.03.30 65th Edition, January 1, 1999
Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle.
Includes all amendments and changes through AA, January 1, 1999

ESDU AERO 00.03.30

65th Edition, January 1, 1999

Complete Document
 
Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle.
Includes all amendments and changes through AA, January 1, 1999
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ESDU AERO 00.03.05 1948 Edition, February 1, 1948
Isentropic expansion of air from rest.

ESDU AERO 00.03.05

1948 Edition, February 1, 1948

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Isentropic expansion of air from rest.
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ESDU AERO A.S.06.03.01 57th Edition, October 1, 1982
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO A.S.06.03.01

57th Edition, October 1, 1982

Complete Document
 
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO B.S.02.03.01 54th Edition, January 1, 1981
Introductory notes on the drag at zero incidence of bodies at supersonic speeds.
Includes all amendments and changes through AC, January 1, 1981

ESDU AERO B.S.02.03.01

54th Edition, January 1, 1981

Complete Document
 
Introductory notes on the drag at zero incidence of bodies at supersonic speeds.
Includes all amendments and changes through AC, January 1, 1981
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ESDU AERO A.S.02.03.01 59th Edition, May 1, 1975
Explanatory notes on transonic and supersonic area rules.
Includes all amendments and changes through AB, May 1, 1975

ESDU AERO A.S.02.03.01

59th Edition, May 1, 1975

Complete Document
 
Explanatory notes on transonic and supersonic area rules.
Includes all amendments and changes through AB, May 1, 1975
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ESDU AERO B.S.05.03.01 54th Edition, March 1, 1980
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
Includes all amendments and changes through AA, March 1, 1980

ESDU AERO B.S.05.03.01

54th Edition, March 1, 1980

Complete Document
 
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
Includes all amendments and changes through AA, March 1, 1980
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ESDU AERO S.00.03.16 54th Edition, March 1, 1975
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on wedges.
Includes all amendments and changes through AB, March 1, 1975

ESDU AERO S.00.03.16

54th Edition, March 1, 1975

Complete Document
 
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on wedges.
Includes all amendments and changes through AB, March 1, 1975
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ESDU AERO S.00.03.23 59th Edition, June 1, 1982
Conditions behind oblique shock waves for air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982

ESDU AERO S.00.03.23

59th Edition, June 1, 1982

Complete Document
 
Conditions behind oblique shock waves for air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982
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ESDU AERO S.00.03.22 59th Edition, June 1, 1982
Conditions behind normal shock waves in air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982

ESDU AERO S.00.03.22

59th Edition, June 1, 1982

Complete Document
 
Conditions behind normal shock waves in air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982
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ESDU AERO S.00.03.14 53rd Edition, March 1, 1995
Approximate calculation of the pressure changes in two-dimensional supersonic flow.
Includes all amendments and changes through AB, March 1, 1995

ESDU AERO S.00.03.14

53rd Edition, March 1, 1995

Complete Document
 
Approximate calculation of the pressure changes in two-dimensional supersonic flow.
Includes all amendments and changes through AB, March 1, 1995
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ESDU AERO S.00.03.13 54th Edition, May 1, 1975
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones.
Includes all amendments and changes through AB, May 1, 1975

ESDU AERO S.00.03.13

54th Edition, May 1, 1975

Complete Document
 
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones.
Includes all amendments and changes through AB, May 1, 1975
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